Rankers Physics
Topic: Solid and Fluids
Subtopic: Fluid Dynamics

A fully loaded Boeing aircraft has a mass of \[3.3\times 10^{5} kg\]. Its total wing area is 500 m2. It is in level flight with speed of 960 kmph. Estimate the pressure difference between the lower and upper surfaces of the wings :
\[4.5\times 10^{3} N/m^{-2}\]
\[5.5\times 10^{3} N/m^{-2}\]
\[6.6\times 10^{3} N/m^{-2}\]
\[7.5\times 10^{3} N/m^{-2}\]

No solution provided for this question.

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